PPRuNe Forums - View Single Post - Blade pitch stall margin
View Single Post
Old 4th Sep 2003, 11:25
  #1 (permalink)  
Join Date: Jul 2003
Location: Port Townsend,WA. USA
Posts: 440
Blade pitch stall margin

The Robinson R22 flight manual states the blade pitch is near stall at higher gross weight. Also the NTSB special report on the R22 accident history dicusses the high blade pitch of the Robinson as a possible cause of the several dozen rotor separation incidents.
My question is: what is the blade pitch of a R22 in hover and cruise and what is the blade pitch of other helicopters. Is it normal to run close to blade stall?
slowrotor is offline